Performance of Transpiration-Cooled Heat Shields for Reentry Vehicles
Author:
Affiliation:
1. University of Oxford, Oxford, England OX2 0ES, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference53 articles.
1. Hypersonic and High-Temperature Gas Dynamics, Second Edition
2. Flowfield and Pressure Decay Analysis of Porous Cones
3. Experimental Investigation on Transpiration Cooling Effectiveness for Spacecraft Entering Martian Atmosphere
4. Transpiration-Cooled Hypersonic Flight Experiment: Setup, Flight Measurement, and Reconstruction
5. Application of Transpiration Cooling for Hot Structures
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